The invention provides an aircraft stand-alone structure health monitoring system, and belongs to the technical field of aircraft structure health monitoring. The system comprises a sensor assembly, a structure health monitoring computer, a task machine, a light voice alarm computer, a light voice alarm assembly, a flight control computer and a control stick shaking assembly. The sensor assembly is connected with the structure health monitoring computer through a bus, the structure health monitoring computer, the light voice alarm computer and the flight control computer are connected with the task machine through a bus, the light voice alarm computer is electrically connected with the light voice alarm assembly, and the flight control computer is electrically connected with the control stick shaking assembly. An intelligent sensor is used for sensing the loading and health conditions of key parts of an aircraft structure, the health conditions of the key parts of the structure are informed to a pilot in real time, the pilot can adjust the flight attitude conveniently, and man-machine safety is guaranteed; the data collected by the sensor are combined with an algorithm to predict the fault occurrence of the aircraft structure, and single-machine health monitoring can be carried out to further guarantee the safety of the aircraft structure.
本发明提供一种飞机单机结构健康监控系统,属于飞机结构健康监控技术领域。该系统包括传感器组件、结构健康监控计算机、任务机、灯光语音告警计算机、灯光语音告警组件、飞控计算机、驾驶杆抖杆组件。传感器组件与结构健康监控计算机、结构健康监控计算机、灯光语音告警计算机和飞控计算机与任务机均用总线连接,灯光语音告警计算机与灯光语音告警组件、飞控计算机与驾驶杆抖杆组件均用电连接。本发明应用智能传感器感知飞机结构关键部位受载和健康情况,将结构关键部位的健康状况实时告知飞行员,便于飞行员调整飞行姿态,保障人机安全;传感器采集的数据结合算法可以预测飞机结构故障发生,也可以开展单机健康监控,进一步保障飞机结构的安全。
Airplane stand-alone structure health monitoring system
一种飞机单机结构健康监控系统
2021-10-22
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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